Electrical current generation system

ABSTRACT

An electrical generating system consists of a fuel cell, and an oxygen gas delivery. The fuel cell includes and anode channel having an anode gas inlet for receiving a supply of hydrogen gas, a cathode channel having a cathode gas inlet and a cathode gas outlet, and an electrolyte in communication with the anode and cathode channel for facilitating ion exchange between the anode and cathode channel. The oxygen gas delivery system is coupled to the cathode gas inlet and delivers oxygen gas to the cathode channel. The electrical current generating system also includes gas recirculation means couple to the cathode gas outlet for recirculating a portion of cathode exhaust gas exhausted from the cathode gas outlet to the cathode gas inlet.

CROSS REFERENCE TO RELATED APPLICATIONS

The present application is a continuation-in-part of prior internationalapplication No. PCT/CA99/00823, filed Sep. 14, 1999, which claimedpriority from U.S. provisional application No. 60/100,091, filed Sep.14, 1998, and Canadian patent application No. 2,274,240, filed Jun. 10,1999, which applications are incorporated herein by reference.

FIELD

The present invention relates to a fuel cell for the generation ofelectrical current. In particular, the present invention relates to afuel cell-based electrical generation system which employs pressureswing adsorption for enhancing the efficiency of the fuel cell.

BACKGROUND

Fuel cells provide an environmentally friendly source of electricalcurrent. One form of fuel cell used for generating electrical powerincludes an anode for receiving hydrogen gas, a cathode for receivingoxygen gas, and an alkaline electrolyte. Another form of fuel cellincludes an anode channel for receiving a flow of hydrogen gas, acathode channel for receiving a flow of oxygen gas, and a polymerelectrolyte membrane (PEM) which separates the anode channel from thecathode channel. In both instances, oxygen gas which enters the cathodereacts with hydrogen ions which cross the electrolyte to generate a flowof electrons. Environmentally safe water vapor is also produced as abyproduct. However, several factors have limited the widespread use offuel cells as power generation systems.

In order to extract a continuous source of electrical power from a fuelcell, it is necessary to provide the fuel cell with a continuous sourceof oxygen and hydrogen gas. However, with atmospheric air as the directsource of oxygen to the cathode channel, performance of PEM fuel cellsis severely impaired by the low partial pressure of oxygen and theconcentration polarization of nitrogen, while alkaline fuel cellsrequire a pretreatment purification system to remove carbon dioxide fromthe feed air. Further, as the average oxygen concentration in a cathodechannel with atmospheric air feed is typically only about 15%, the sizeof the fuel cell must be undesirably large in order to providesufficient power for industrial applications.

In order to achieve a partial pressure of oxygen through the cathodechannel sufficient for the attainment of competitive current densitiesfrom a PEM fuel cell system, particularly for vehicular propulsion, itis necessary to compress the air feed to at least 3 atmospheres beforethe air feed is introduced to the cathode channel. As will beappreciated, the power input necessary to sufficiently compress the airfeed reduces the overall efficiency of the fuel cell system. It has beenproposed to use polymeric membranes to enrich the oxygen, but suchmembranes actually reduce the oxygen partial pressure and the reductionin total pressure more than offsets the limited enrichment attainable.

External production, purification, dispensing and storage of hydrogen(either as compressed gas or cryogenic liquid) requires costlyinfrastructure, while storage of hydrogen fuel on vehicles presentsconsiderable technical and economic barriers. Accordingly, forstationary power generation, it is preferred to generate hydrogen fromnatural gas by steam reforming or partial oxidation followed by watergas shift. For fuel cell vehicles using a liquid fuel, it is preferredto generate hydrogen from methanol by steam reforming or from gasolineby partial oxidation of autothermal reforming, again followed by watergas shift. However, the resulting hydrogen contains carbon monoxide andcarbon dioxide impurities which cannot be tolerated respectively by thePEM fuel cell catalytic electrodes and the alkaline fuel cellelectrolyte in more than trace levels.

In prior art PEM fuel cells operating with an autothermal or partialoxidation fuel processor, ambient air is used as the oxidant. Thisresults in a large load of nitrogen having to be heated and then cooledthrough the fuel processor system. The substantial volume of nitrogencontributes to pressure losses throughout the fuel processor and anodechannels, or alternatively to the cost and physical bulk penalties ofmaking those passages larger.

While water recovery from fuel cell exhaust is highly desirable forefficient fuel processor operation, the conventional fuel celldischarges its oxygen-depleted cathode exhaust gas to atmosphere, andthus requires an extra condenser to recover water which then must bevaporized in the fuel processor at a substantial energy cost. Thiscondenser adds to the radiator cooling load which is already a problemfor automotive fuel cell power plants in view of the large amount of lowgrade heat which must be rejected.

The conventional method of removing residual carbon monoxide from thehydrogen feed to PEM fuel cells has been catalytic selective oxidation,which compromises efficiency as both the carbon monoxide and a fractionof the hydrogen are consumed by low temperature oxidation, without anyrecovery of the heat of combustion. Palladium diffusion membranes can beused for hydrogen purification, but have the disadvantages of deliveryof the purified hydrogen at low pressure, and also the use of rare andcostly materials.

Pressure swing adsorption systems (PSA) have the attractive features ofbeing able to provide continuous sources of oxygen and hydrogen gas,without significant contaminant levels. PSA systems and vacuum pressureswing adsorption systems (vacuum-PSA) separate gas fractions from a gasmixture by coordinating pressure cycling and flow reversals over anadsorbent bed which preferentially adsorbs a more readily adsorbed gascomponent relative to a less readily adsorbed gas component of themixture. The total pressure of the gas mixture in the adsorbent bed iselevated while the gas mixture is flowing through the adsorbent bed froma first end to a second end thereof, and is reduced while the gasmixture is flowing through the adsorbent from the second end back to thefirst end. As the PSA cycle is repeated, the less readily adsorbedcomponent is concentrated adjacent the second end of the adsorbent bed,while the more readily adsorbed component is concentrated adjacent thefirst end of the adsorbent bed. As a result, a “light” product (a gasfraction depleted in the more readily adsorbed component and enriched inthe less readily adsorbed component) is delivered from the second end ofthe bed, and a “heavy” product (a gas fraction enriched in the morestrongly adsorbed component) is exhausted from the first end of the bed.

However, the conventional system for implementing pressure swingadsorption or vacuum pressure swing adsorption uses two or morestationary adsorbent beds in parallel, with directional valving at eachend of each adsorbent bed to connect the beds in alternating sequence topressure sources and sinks. This system is often difficult and expensiveto implement due to the complexity of the valving required.

Further, the conventional PSA system makes inefficient use of appliedenergy, because feed gas pressurization is provided by a compressorwhose delivery pressure is the highest pressure of the cycle. In PSA,energy expended in compressing the feed gas used for pressurization isthen dissipated in throttling over valves over the instantaneouspressure difference between the absorber and the high pressure supply.Similarly, in vacuum-PSA, where the lower pressure of the cycle isestablished by a vacuum pump exhausting gas at that pressure, energy isdissipated in throttling over valves during countercurrent blowdown ofadsorbers whose pressure is being reduced. A further energy dissipationin both systems occurs in throttling of light reflux gas used for purge,equalization, concurrent blowdown and product pressurization or backfillsteps. These energy sinks reduce the overall efficiency of the fuel cellsystem.

Additionally, conventional PSA systems can generally only operate atrelatively low cycle frequencies, necessitating the use of largeadsorbent inventories. The consequent large size and weight of such PSAsystems renders them unsuitable for vehicular fuel cell applications.Thus, a conventional PSA unit for oxygen concentration would require anadsorbent bed volume of about 400 L, and an additional installed volumeof about 100 L for pressure enclosures and PSA cycle control valves, inorder to deliver a product flow containing about 200 L/min oxygen whichwould be sufficient for a 40 kW fuel cell.

Accordingly, there remains a need for an efficient fuel cell-basedelectrical generation system which can produce sufficient power forindustrial applications and which is suitable for vehicularapplications. There also remains a need for compact, lightweighthydrogen and oxygen PSA systems that operate at higher cycle frequenciesand are suitable for vehicular fuel cell-based applications.

SUMMARY OF THE INVENTION

According to the invention, there is provided a fuel cell-basedelectrical generation system which addresses the deficiencies of theprior art fuel cell electrical generation systems.

The electrical current generating system, according to a firstembodiment of the present invention, comprises a fuel cell, and anoxygen gas delivery system. The fuel cell includes an anode channelhaving an anode gas inlet for receiving a supply of hydrogen gas, acathode channel having a cathode gas inlet and a cathode gas outlet, andan electrolyte in communication with the anode and cathode channel forfacilitating ion exchange between the anode and cathode channel. Theoxygen gas delivery system is coupled to the cathode gas inlet anddelivers oxygen gas to the cathode channel.

The electrical current generating system also includes gas recirculationmeans coupled to the cathode gas outlet for recirculating a portion ofcathode exhaust gas (which is still enriched in oxygen relative toambient air, and carries fuel cell exhaust water and fuel cell wasteheat) from the cathode gas outlet to the cathode gas inlet.

In some embodiments, at least a portion of the cathode exhaust gas isreturned to the inlet of an autothermal or partial oxidation fuelprocessor (or reformer) for reacting a hydrocarbon fuel with oxygen andsteam in order to generate raw hydrogen or syngas.

In a preferred implementation of the first embodiment, the oxygen gasdelivery system comprises an oxygen gas separation system for extractingenriched oxygen gas from air. Preferably, the oxygen gas separatingsystem comprises an oxygen pressure swing adsorption system including arotary module having a stator and a rotor rotatable relative to thestator. The rotor includes a number of flow paths for receivingadsorbent material therein for preferentially adsorbing a first gascomponent in response to increasing pressure in the flow paths relativeto a second gas component. The pressure swing adsorption system alsoincludes compression machinery coupled to the rotary module forfacilitating gas flow through the flow paths for separating the firstgas component from the second gas component. The stator includes a firststator valve surface, a second stator valve surface, and plurality offunction compartments opening into the stator valve surfaces. Thefunction compartments include a gas fee compartment, a light reflux exitcompartment and a light reflux return compartment.

In one variation, the compression machinery comprises a compressor fordelivering pressurized air to the gas feed compartment, and a lightreflux expander coupled between the light reflux exit compartment andthe light reflux compartment. The gas recirculating means comprises acompressor coupled to the light reflux expander for supplying oxygengas, exhausted from the cathode gas outlet, under pressure to thecathode gas inlet. As a result, energy recovered from the pressure swingadsorption system can be applied to boost the pressure of oxygen gasdelivered to the cathode gas inlet.

In another variation, restrictor orifices are disposed between the lightreflux exit compartment and the light reflux return compartment forpressure letdown in replacement of the light reflux expander. The gasrecirculating means comprises a compressor coupled to the cathode gasoutlet for supplying oxygen gas to the cathode gas inlet, and arestrictive orifice disposed between the cathode gas outlet and apressurization compartment for recycling a portion of the oxygen gas asfeed gas to the pressure swing adsorption system. As a result, energyrecovered from the cathode gas outlet can be used to help pressurize thecathode gas inlet through the PSA system.

The electrical current generating system, according to a secondembodiment of the present invention, comprises a fuel cell, an oxygengas delivery system, and a hydrogen gas delivery system. The fuel cellincludes an anode channel having an anode gas inlet and an anode gasoutlet, a cathode channel having a cathode gas inlet and a cathode gasoutlet, and an electrolyte in communication with the anode and cathodechannel for facilitating ion exchange between the anode and cathodechannel.

The oxygen gas delivery system is coupled to the cathode gas inlet anddelivers oxygen gas to the cathode channel. The hydrogen gas deliverysystem includes a hydrogen gas inlet for receiving a first hydrogen gasfeed from the anode gas outlet, and a hydrogen gas outlet coupled to theanode gas inlet for delivering hydrogen gas received from the firsthydrogen gas feed to the anode channel with increased purity.

In a preferred implementation of the second embodiment, the oxygen gasseparation system comprises an oxygen pressure swing adsorption system,and the hydrogen gas separation system comprises a reactor for producinga second hydrogen gas fee from hydrocarbon fuel, and a hydrogen pressureswing adsorption system coupled to the reactor for purifying hydrogengas received from the first and second hydrogen gas feeds. Both pressureswing adsorption systems include a rotary module having a stator and arotor rotatable relative to the stator. The rotor includes a number offlow paths for receiving adsorbent material therein for preferentiallyadsorbing a first gas component in response to increasing pressure inthe flow paths relative to a second gas component. The functioncompartments include a gas feed compartment and a heavy productcompartment.

In one variation, the oxygen pressure swing adsorption system includes acompressor coupled to the gas feed compartment for deliveringpressurized air to the gas feed compartment, and a vacuum pump coupledto the compressor for extracting nitrogen product gas from the heavyproduct compartment. The reactor comprises a steam reformer, including aburner, for producing syngas, and a water gas shift reactor coupled tothe steam reformer for converting the syngas to the second hydrogen gasfeed. The hydrogen pressure swing adsorption system includes a vacuumpump for delivering fuel gas from the heavy product compartment to theburner. The fuel gas is burned in the burner, and the heat generatedtherefrom is used to supply the endothermic heat of reaction necessaryfor the steam reformer reaction. The resulting syngas is delivered tothe water gas shift reactor for removal of impurities, and thendelivered as the second hydrogen gas feed to the hydrogen pressure swingadsorption system.

In another variation, the invention includes a burner for burning fuel.The reactor comprises an autothermal reformer for producing syngas, anda water gas shift reactor coupled to the autothermal reformer forconverting the syngas to the second hydrogen gas fee. The compressor ofthe oxygen pressure swing adsorption system delivers pressurized air tothe burner, and the heavy product gas is delivered from the hydrogenpressure swing adsorption system as tail gas to be burned in the burner.The compression machine of the oxygen pressure swing adsorption systemalso includes an expander coupled to the compressor for driving thecompressor from hot gas of combustion emitted from the burner. Heat fromthe burner may also be used to preheat air and/or fuel supplied to theautothermal reformer.

BRIEF DESCRIPTION OF THE DRAWINGS

The preferred embodiment of the present invention will now be described,by way of example only, with reference to the drawings, in which:

FIG. 1 is a sectional view of a rotary PSA module suitable for use withthe present invention, showing the stator and rotor situated in thestator.

FIG. 2 is a sectional view of the module of FIG. 1, with the statordeleted for clarity.

FIG. 3 is a sectional view of the stator shown in FIG. 1, with the rotordeleted for clarity.

FIG. 4 is an axial section of the module of FIG. 1.

FIG. 5 shows a typical PSA cycle attainable with the PSA system shown inFIGS. 1 to 4.

FIG. 6 shows one variation of the PSA cycle with heavy reflux,attainable with the PSA system shown in FIGS. 1 to 4.

FIG. 7 shows a pressure swing adsorption apparatus for separating oxygengas from air, suitable for use with the present invention, and depictingthe rotary module shown in FIG. 1 and a compression machine coupled tothe rotary module.

FIG. 8 shows a pressure swing adsorption apparatus for purifyinghydrogen gas, suitable for use with the present invention, and depictingthe rotary module shown in FIG. 1 and a compression machine coupled tothe rotary module.

FIG. 9 shows an electrical current generating system, according to afirst embodiment of the present invention, including anoxygen-separating PSA system for supplying enriched oxygen to the fuelcell cathode channel with energy recovery from light reflux expansion toboost the pressure of oxygen circulating in the fuel cell cathode loop.

FIG. 10 shows a first variation of the electrical current generatingsystem shown in FIG. 9, but with the PSA system including acountercurrent blowdown expander driving a free rotor exhaust vacuumpump for vacuum-PSA operation.

FIG. 11 shows a second variation of the electrical current generatingsystem shown in FIG. 9, with a portion of the oxygen enriched gasdischarged from the fuel cell cathode being used for a pressurizationstep for the PSA system.

FIG. 12 shows an electrical current generating system, according to asecond embodiment of the present invention, including anoxygen-separating PSA system for supplying enriched oxygen to the fuelcell cathode channel, and a hydrogen-separating PSA system for supplyingenriched hydrogen to the fuel cell anode channel, with thehydrogen-separating PSA system receiving feed gas from a streamreformer.

FIG. 13 shows an electrical current generating system, according to avariation of the electrical current generating system shown in FIG. 12,but with the hydrogen-separating PSA system receiving feed gas from anautothermal reformer.

FIG. 14 shows an electrical current generating system with carbondioxide removal and oxygen enrichment for an alkaline fuel cell, andwith an oxygen accumulator.

FIG. 15 shows an axial section of a rotary PSA module with rotatingadsorbers and stationary distributor valves.

FIG. 16 shows a transverse section of the module of FIG. 15.

FIG. 17 shows a transverse section of the module of FIG. 15.

FIG. 18 shows a transverse section of the module of FIG. 15.

FIG. 19 shows a transverse section of the module of FIG. 15.

FIG. 20 shows a transverse section of the module of FIG. 15.

FIG. 21 shows a transverse section of the module of FIG. 15.

FIG. 22 shows an axial section of a rotary PSA module with stationaryadsorbers and rotating distributor valves.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

To aid in understanding the present invention, a pressure swingadsorption process and associated apparatus, suitable for use with thepresent invention, will be described first, with reference to FIGS. 1through 6. Thereafter, an oxygen-separating pressure swing adsorptionsystem and a hydrogen-separating pressure swing adsorption system willbe described with reference to FIGS. 7 and 8 respectively. Twoembodiments of the invention, together with variations thereon, willthen be described commencing with FIG. 9.

FIGS. 1, 2, 3 and 4

A rotary module 10 which is suitable for use as part of the presentinvention is shown in FIGS. 1, 2, 3 and 4. The module includes a rotor11 revolving about axis 12 in the direction shown by arrow 13 withinstator 14. However, it should be understood that the invention is notlimited to PSA systems having rotary modules. Rather other arrangementsmay be employed without departing from the scope of the invention. Forinstance, if desired, the present invention may be employed withmultiple stationary adsorbent beds in parallel, with directional valvingat each of each adsorbent bed to connect the beds in alternatingsequence to pressure sources and sinks. However, as will becomeapparent, the rotary module 10 is preferred since it provides highlydesirable features of efficiency and compactness.

Rotary PSA modules include those with rotating absorber modules toprovide the rotary valve function, and those with a fixed absorbermodule cooperating with rotating valves, preferably coaxial to theabsorber module. In a particular embodiment, the rotary PSA module is acylindrical axial flow absorber module, with feed and product rotaryvalve faces at opposite ends of the absorber module. The absorber modulemay rotate or remain stationary, the later version including fluidtransfer between the casing and the rotating valve rotors.

In general, the rotary module 10 may be configured for flow through theabsorber elements in the radial, axial or oblique conical directionsrelative to the rotor axis. For operation at high cycle frequency,radial flow has the advantage that the centripetal acceleration will lieparallel to the flow path for most favorable stabilization ofbuoyancy-driven free convection. Radial flow configurations may bepreferred for large module capacities.

Axial flow configurations may be preferred for smaller modulecapacities, and advantageously allow increased compactness of fuel cellsystems that incorporate PSA systems, at least for smaller power ratingsbelow about 300 kW. Compactness is an important consideration forenabling practicable use of PSA systems in automotive fuel cell powerplants.

As shown in FIG. 2, the rotor 11 is of annular section, havingconcentrically to axis 12 an outer cylindrical wall 20 whose externalsurface is first valve surface 21, and an inner cylindrical wall 22whose internal surface is second valve surface 23. The rotor has (in theplane of the section defined by arrows 15 and 16 in FIG. 4) a total of“N” radial flow absorber elements 24. An adjacent pair of absorberelements 25 and 26 are separated by partition 27 which is structurallyand sealingly joined to outer wall 20 and inner wall 22. Adjacentabsorber elements 25 and 26 are angularly spaced relative to axis 12 byan angle of 360°/N. Since the absorber elements and the valve surfacesare thereby integrated into a single unit, and the absorber elements arelocated in close proximity to the valve surfaces with minimal deadvolume, the rotary module 10 is more compact and efficient thanconventional PSA systems.

Absorber element 24 has a first end 30 defined by support screen 31 anda second end 32 defined by support screen 33. The absorber may beprovided as granular adsorbent, whose packing voidage defines a flowpath contacting the adsorbent between the first and second ends of theabsorber. However, as described in copending U.S. patent applicationSer. No. 08/995,906, the description therein being incorporated hereinby reference, preferably the absorber element is provided as an array oflaminated thin sheets extending between the first and second ends of theabsorber, the sheets having an adsorbent such as a zeolite supported ona reinforcement matrix, and with flow channels established by spacersbetween the sheets. The laminated sheet absorber, with sheet thicknessof approximately 150 microns and using type X zeolites, has greatlyreduced mass transfer and pressure drop resistances compared toconventional granular adsorbers, so that satisfactory oxygen enrichmentoperation has been achieved with PSA cycle periods in the order of 1second and as low as 0.4 second. Consequently, the adsorbent inventoryis radically reduced compared to conventional PSA cycle periods of about1 minute, with the size of the module being smaller by some two ordersof magnitude compared to conventional PSA equipment of equivalentcapacity. As a result, an exceptionally compact PSA module that can beused, rendering the invention particularly suitable for vehicular fuelcell power plants.

First aperture or orifice 34 provides flow communication from firstvalve surface 21 through wall 20 to the first end 30 of absorber 24.Second aperture or orifice 35 provides flow communication from secondvalve surface 23 through wall 22 to the second end 31 of absorber 24.Support screens 31 and 33 respectively provide flow distribution 32between first aperture 34 and first end 30, and between second aperture35 and second end 32, of absorber element 24.

As shown in FIG. 3, stator 14 is a pressure housing including an outercylindrical shell or first valve stator 40 outside the annular rotor 11,and an inner cylindrical shell or second valve stator 41 inside theannular rotor 11. Outer shell 40 carries axially extending strip seals(e.g. 42 and 43) sealingly engaged with first valve surface 21, whileinner shell 41 carries axially extending strip seals (e.g. 44 and 45)sealingly engaged with second valve surface 23. Preferably, theazimuthal sealing width of the strip seals is greater than the diametersor azimuthal widths of the first and second apertures 34 and 35 openingthrough the first and second valve surfaces.

A set of first compartments in the outer shell each open in an annularsector to the first valve surface, and each provide fluid communicationbetween its angular sector of the first valve surface and a manifoldexternal to the module. The angular sectors of the compartments are muchwider than the angular separation of the absorber elements. The firstcompartments are separated on the first sealing surface by the stripseals (e.g. 42). Proceeding clockwise in FIG. 3, in the direction ofrotor rotation, a first feed pressurization compartment 46 communicatesby conduit 47 to first feed pressurization manifold 48, which ismaintained at a first intermediate feed pressure. Similarly, a secondfeed pressurization compartment 50 communicates to second feedpressurization manifold 51, which is maintained at a second intermediatefeed pressure higher than the first intermediate feed pressure but lessthan the higher working pressure.

For greater generality, module 10 is shown with provision for sequentialadmission of two feed mixtures, the first feed gas having a lowerconcentration of the more readily adsorbed component relative to thesecond feed gas. First feed compartment 52 communicates to first feedmanifold 53, which is maintained at substantially the higher workingpressure. Likewise, second feed compartment 54 communicates to secondfeed manifold 55, which is maintained at substantially the higherworking pressure. A first countercurrent blowdown compartment 56communicates to first countercurrent blowdown manifold 57, which ismaintained at a first countercurrent blowdown intermediate pressure. Asecond countercurrent blowdown compartment 58 communicates to secondcountercurrent blowdown manifold 59, which is maintained at a secondcountercurrent blowdown intermediate pressure above the lower workingpressure. A heavy product compartment 60 communicates to heavy productexhaust manifold 61 which is maintained at substantially the lowerworking pressure. It will be noted that compartment 58 is bounded bystrip seals 42 and 43, and similarly all the compartments are boundedand mutually isolated by strip seals.

A set of second compartments in the inner shell each open in an angularsector to the second valve surface, and each provide fluid communicationbetween its angular sector of the second valve surface and a manifoldexternal to the module. The second compartments are separated on thesecond sealing surface by the strip seals (e.g. 44). Proceedingclockwise in FIG. 3, again in the direction of rotor rotation, lightproduct compartment 70 communicates to light product manifold 71, andreceives high product gas at substantially the higher working pressure,less frictional pressure drops through the adsorbers and the first andsecond orifices. According to the angular extension of compartment 70relative to compartment 52 and 54, the light product may be obtainedonly from adsorbers simultaneously receiving the first feed gas fromcompartment 52, or from adsorbers receiving both the first and secondfeed gases.

A first light reflux exit compartment 72 communicates to first lightreflux exit manifold 73, which is maintained at a first light refluxexit pressure, here substantially the higher working pressure lessfrictional pressure drops. A first concurrent blowndown compartment 74(which is actually the second light reflux exit compartment),communicates to second light reflux exit manifold 75, which ismaintained at a first concurrent blowdown pressure less than the higherworking pressure. A second concurrent blowdown compartment or thirdlight reflux exit compartment 76 communicates to third light reflux exitmanifold 77, which is maintained at a second concurrent blowdownpressure less than the first concurrent blowdown pressure. A thirdconcurrent blowdown compartment or fourth light reflux exit compartment78 communicates to fourth light reflux exit manifold 79, which ismaintained at a third concurrent blowdown pressure less than the secondconcurrent blowdown pressure.

A purge compartment 80 communicates to a fourth light reflux returnmanifold 81, which supplies the fourth light reflux gas which has beenexpanded form the third concurrent blowdown pressure to substantiallythe lower working pressure with an allowance for frictional pressuredrops. The ordering of light reflux pressurization steps is invertedfrom the ordering or light reflux exit or concurrent blowdown steps, soas to maintain a desirable “last out—first in” stratification of lightreflux gas packets. Hence a first light reflux pressurizationcompartment 82 communicates to a third light reflux return manifold 83,which supplies the third light reflux gas which has been expanded fromthe second concurrent blowdown pressure to a first light refluxpressurization pressure greater than the lower working pressure. Asecond light reflux pressurization compartment 84 communicates to asecond light reflux return manifold 85, which supplies the second lightreflux gas which has been expanded from the first concurrent blowdownpressure to a second light reflux pressurization pressure greater thanthe first light reflux pressurization pressure. Finally, a third lightreflux pressurization compartment 86 communicates to a first lightreflux return manifold 87, which supplies the first light reflux gaswhich has been expanded from approximately the higher pressure to athird light reflux pressurization pressure greater than the second lightreflux pressurization pressure, and in this example less than the firstfeed pressurization pressure.

Additional details are shown in FIG. 4. Conduits 88 connect firstcompartment 60 to manifold 61, with multiple conduits providing for goodaxial flow distribution in compartment 60. Similarly, conduits 89connect second compartment 80 to manifold 81. Stator 14 has base 90 withbearings 91 and 92. Motor 95 is coupled to shaft 94 to drive rotor 11.The rotor could alternatively rotate as an annular drum, supported byrollers at several angular positions about its rim and also driven atits rim so that no shaft would be required. A rim drive could beprovided by a ring gear attached to the rotor, or by a linearelectromagnetic motor whose stator would engage an arc of the rim.Particularly for hydrogen separation applications, the rotor drive maybe hermetically enclosed within the stator housing to eliminate hazardsrelated to seal leakage. Outer circumferential seals 96 seal the ends ofouter strip seals 42 and the edges of first valve surface 21, whileinner circumferential seals 97 seal the ends of inner strip seals 44 andthe edges of second valve surface 23. Rotor 11 has access plug 98between outer wall 20 and inner wall 22, which provides access forinstallation and removal of the adsorbent in adsorbers 24.

FIGS. 5 and 6

FIG. 5 shows a typical PSA cycle which would be obtained using theforegoing gas separation system, while FIG. 6 shows a similar PSA cyclewith heavy reflux recompression of a portion of the first product gas toprovide a second feed gas to the process.

In FIGS. 5 and 6, the vertical axis 150 indicates the working pressurein the adsorbers and the pressure in the first and second compartments.Pressure drops due to flow within the absorber elements are neglected.The higher and lower working pressures are respectively indicated bydotted lines 151 and 152. The lower working pressure may be nominally orapproximately ambient atmospheric pressure, or may be a subatmosphericpressure established by vacuum pumping. The higher working pressure maytypically be in the range of twice to four times the lower workingpressure, based on the ratio of absolute pressures.

The horizontal axis 155 of FIGS. 5 and 6 indicates time, with the PSAcycle period defined by the time interval between points 156 and 157. Attimes 156 and 157, the working pressure in a particular absorber ispressure 158. Starting from time 156, the cycle for a particularabsorber (e.g. 24) begins as the first aperture 34 of that absorber isopened to the first feed pressurization compartment 46, which is fed byfirst feed supply means 160 at the first intermediate feed pressure 161.The pressure in that absorber rises from pressure 158 at time 157 to thefirst intermediate feed pressure 161. Proceeding ahead, first aperturepasses over a seal strip, first closing absorber 24 to compartment 46and then opening it to second feed pressurization compartment 50 whichis feed by second feed supply means 162 at the second intermediate feedpressure 163. The absorber pressure rises to the second intermediatefeed pressure.

First aperture 34 of absorber 24 is opened next to first feedcompartment 52, which is maintained at substantially the higher pressureby a third feed supply means 165. Once the absorber pressure has risento substantially the higher working pressure, its second aperture 35(which has been closed to all second compartments since time 156) opensto light product compartment 70 and delivers light product 166.

In the cycle of FIG. 6, first aperture 34 of absorber 24 is opened nextto second feed compartment 54, also maintained at substantially thehigher pressure by a fourth feed supply means 167. In general, thefourth feed supply means supplies a second feed gas, typically richer inthe more readily adsorbed component than the first feed gas provided bythe first, second and third feed supply means. In the specific cycleillustrated in FIG. 6, the fourth feed supply means 167 is a “heavyreflux” compressor, recompressing a portion of the heavy product backinto the apparatus. In the cycle illustrated in FIG. 5, there is nofourth feed supply means, and compartment 54 could be eliminated orconsolidated with compartment 52 extended over a wider angular arc tothe stator.

While feed gas is still being supplied to the first end of absorber 24from either compartment 52 or 54, the second end of absorber 24 isclosed to light product compartment 70 and opens to first reflux exitcompartment 72 while delivering “light reflux” gas (enriched in the lessreadily adsorbed component, similar to second product gas) to firstlight reflux pressure let-down means (or expander) 170. The firstaperture 34 of absorber 24 is then closed to all first compartments,while the second aperture 35 is opened successively to (a) second lightreflux exit compartment 74, dropping the absorber pressure to the firstconcurrent blowdown pressure 171 while delivering light reflux gas tosecond light reflux pressure letdown means 172, (b) third light refluxexit compartment 76, dropping the absorber pressure to the secondconcurrent blowdown pressure 173 while delivering light reflux gas tothird light reflux pressure letdown means 174, and (c) fourth lightreflux exit compartment 78, dropping the absorber pressure to the thirdconcurrent blowdown pressure 175 while delivering light reflux gas tofourth light reflux pressure letdown means 176. Second aperture 35 isthen closed for an interval, until the light reflux return stepsfollowing the countercurrent blowdown steps.

The light reflux pressure let-down means may be mechanical expanders orexpansion stages for expansion energy recovery, or may be restrictororifices or throttle valves for irreversible pressure let-down.

Either when the second aperture is closed after the final light refluxexit step (as shown in FIGS. 5 and 6), or earlier while light refluxexit steps are still underway, first aperture 34 is opened to firstcountercurrent blowdown compartment 56, dropping the absorber pressureto the first countercurrent blowdown intermediate pressure 180 whilereleasing “heavy” gas (enriched in the more strongly adsorbed component)to first exhaust means 181. Then, first aperture 34 is opened to secondcountercurrent blowdown compartment 58, dropping the absorber pressureto the first countercurrent blowndown intermediate pressure 182 whilereleasing heavy gas to second exhaust means 183. Finally reaching thelower working pressure, first aperture 34 is opened to heavy productcompartment 60, dropping the absorber pressure to the lower pressure 152while releasing heavy gas to third exhaust means 184. Once the absorberpressure has substantially reached the lower pressure while firstaperture 34 is open to compartment 60, the second aperture 35 opens topurge compartment 80, which receives fourth light reflux gas from fourthlight reflux pressure let-down means 176 in order to displace more heavygas into first product compartment 60.

In FIG. 5, the heavy gas from the first, second and third exhaust meansis delivered as the heavy product 185. In FIG. 6, this gas is partlyreleased as the heavy product 185, while the balance is redirected as“heavy reflux” 187 to the heavy reflux compressor as fourth feed supplymeans 167. Just as light reflux enables an approach to high purity ofthe less readily adsorbed (“light”) component in the light product,heavy reflux enables an approach to high purity of the more readilyadsorbed (“heavy”) component in the heavy product so that high recoveryof the less readily adsorbed (“light”) product can be achieved.

The absorber is then repressurized by light reflux gas after the firstand second apertures close to compartments 60 and 80. In succession,while the first aperture 34 remains closed at least initially, (a) thesecond aperture 35 is opened to first light reflux pressurizationcompartment 82 to raise the absorber pressure to the first light refluxpressurization pressure 190 while receiving third light reflux gas fromthe third reflux pressure letdown means 174, (b) the second aperture 35is opened to second light reflux pressurization compartment 84 to raisethe absorber pressure to the second light reflux pressurization pressure191 while receiving second light reflux gas from the second light refluxpressure letdown means 172, and (c) the second aperture 35 is opened tothird light reflux pressurization compartment 86 to raise the absorberpressure to the third light reflux pressurization pressure 192 whilereceiving first light reflux gas from the first light reflux pressureletdown means 170. Unless feed pressurization has already been startedwhile light reflux return for light reflux pressurization is stillunderway, the process (as based on FIGS. 5 and 6) begins feedpressurization for the cycle after time 157 as soon as the third lightreflux pressurization step has been concluded.

The pressure variation waveform in each absorber would be a rectangularstaircase if there were no throttling in the first and second valves.Such throttling is needed to smooth pressure and flow transients. Inorder to provide balanced performance, preferably all of the absorberelements and the apertures are closely identical to each other.

The rate of pressure change in each pressurization or blowdown step willbe restricted by throttling in ports (or in clearance or labyrinthsealing gaps) of the first and second valve means, or by throttling inthe apertures at first and second ends of the adsorbers, resulting inthe typical pressure waveform depicted in FIGS. 5 and 6. Alternatively,the apertures may be opened slowly by the seal strips, to provide flowrestriction throttling between the apertures and the seal strips, whichmay have narrow tapered clearance channels so that the apertures areonly opened to full flow gradually. Excessively rapid rates of pressurechange would subject the absorber to mechanical stress, while alsocausing flow transients which would tend to increase axial dispersion ofthe concentration wavefront in the absorber. Pulsations of flow andpressure are minimized by having a plurality of adsorbers simultaneouslytransiting each step of the cycle, and by providing enough volume in thefunction compartments and associated manifolds so that they acteffectively as surge adsorbers between the compression machinery and thefirst and second valve means.

It will be evident that the cycle could be generalized in manyvariations by having more or fewer intermediate stages in each majorstep of feed pressurization, countercurrent blowdown exhaust, or lightreflux. If desired, combined feed and product pressurization steps (orcombined concurrent and countercurrent blowdown steps) at intermediatepressures may be performed from both first and second valvessimultaneously. The pressure at which feed pressurization begins, maydiffer from the pressure at which countercurrent blowdown begins.Furthermore, in air separation or air purification applications, a stageof feed pressurization (typically the first stage) could be performed byequalization with atmosphere as an intermediate pressure of the cycle.Similarly, a stage of countercurrent blowdown could be performed byequalization with atmosphere as an intermediate pressure of the cycle.

FIG. 7

FIG. 7 is a simplified schematic of a PSA system for separating oxygenfrom air using nitrogen-selective zeolite adsorbents. The light productis concentrated oxygen, while the heavy product is nitrogen-enriched airusually vented as waste. The cycle lower pressure 152 is illustrated asnominally atmospheric pressure, although a vacuum pressure 152 could beused as will be illustrated in FIG. 8. Feed air is introduced throughfilter intake 200 to a feed compressor 201. The feed compressor includescompressor first stage 202, intercooler 203, compressor second stage204, second intercooler 205, compressor third stage 206, thirdintercooler 207, and compressor fourth stage 208. The feed compressor201 as described may be a four stage axial compressor with motor 209 asprime mover coupled by shaft 210. The intercoolers are optional. Withreference to FIG. 5, the feed compressor first and second stages are thefirst feed supply means 160, delivering feed gas at the firstintermediate feed pressure 161 via conduit 212 and water condensateseparator 213 to first feed pressurization manifold 48. Feed compressorthird stage 206 is the second feed supply means 162, delivering feed gasat the second intermediate feed pressure 163 via conduit 214 and watercondensate separator 215 to second feed pressurization manifold 51. Feedcompressor fourth stage 208 is the third feed supply means 165,delivering feed gas at the higher pressure 151 via conduit 216 and watercondensate separator 217 to feed manifold 53. Light product oxygen flowis delivered from light product manifold 71 by conduit 218, maintainedat substantially the higher pressure less frictional pressure drops.

The PSA system of FIG. 7 includes energy recovery expanders, includinglight reflux expander 220 (here including four stages) andcountercurrent blowdown expander 221 (here including two stages),coupled to feed compressor 201 by shaft 222. The expander stages may beprovided for example as radial inflow turbine stages, as full admissionaxial turbine stages with separate wheels, or as partial admissionimpulse turbine stages combined in a single wheel.

Light reflux gas from first light reflux exit manifold 73 flows at thehigher pressure via conduit 224 and heater 225 to first light pressureletdown means 170 which here is first light reflux expander stage 226,and then flows at the third light reflux pressurization pressure 192 byconduit 227 to the first light reflux return manifold 87. Light refluxgas from second light reflux exit manifold 75 flows at the firstconcurrent blowdown pressure 171 via conduit 228 and heater 225 tosecond light reflux pressure letdown means 172, here the second expanderstage 230, and then flows at the second light reflux pressurizationpressure 191 by conduit 231 to the second light reflux return manifold85. Light reflux gas from third light reflux exit manifold 77 flows atthe second concurrent blowdown pressure 173 via conduit 232 and heater225 to third light reflux pressure pressurization pressure 190 byconduit 235 to the third light reflux return manifold 83. Finally, lightreflux gas from fourth light reflux exit manifold 79 flows at the thirdconcurrent blowdown pressure 175 via conduit 236 and heater 225 tofourth light reflux pressure letdown means 176, here the fourth lightreflux expander stage 238, and then flows at substantially the lowerpressure 152 by conduit 239 to the fourth light reflux return manifold81.

Heavy countercurrent blowdown gas from first countercurrent blowdownmanifold 57 flows at first countercurrent blowdown intermediate pressure180 by conduit 240 to heater 241 and thence to first stage 242 of thecountercurrent blowdown expander 221 as first exhaust means 181, and isdischarged from the expander to exhaust manifold 243 at substantiallythe lower pressure 152. Countercurrent blowdown gas from secondcountercurrent blowdown manifold 59 flows at second countercurrentblowdown intermediate pressure 182 by conduit 244 to heater 241 andthence to second stage 245 of the countercurrent blowdown expander 221as second exhaust means 183, and is discharged from the expander toexhaust manifold 243 at substantially the lower pressure 152. Finally,heavy gas from heavy product exhaust manifold 61 flows by conduit 246 asthird exhaust means 184 to exhaust manifold 243 delivering the heavyproduct gas 185 to be vented at substantially the lower pressure 152.

Optional heaters 225 and 241 raise the temperatures of gases enteringexpanders 220 and 221, thus augmenting the recovery of expansion energyand increasing the power transmitted by shaft 222 from expanders 220 and221 to feed compressor 201, and reducing the power required from primemover 209. While heaters 225 and 241 are means to provide heat to theexpanders, intercoolers 203, 205 and 207 are means to remove heat fromthe feed compressor and serve to reduce the required power of the highercompressor stages. The intercoolers 203, 205, 207 are optional features.

If light reflux heater 249 operates at a sufficiently high temperatureso that the exit temperature of the light reflux expansion stages ishigher than the temperature at which feed gas is delivered to the feedmanifolds by conduits 212, 214 and 216, the temperature of the secondends 35 of the adsorbers 24 may be higher than the temperature of theirfirst ends 34. Hence, the adsorbers have a thermal gradient along theflow path, with higher temperature at their second end relative to thefirst end. This is an extension of the principle of thermally coupledpressure swing adsorption” (TCPSA), introduced by Keefer in U.S. Pat.No. 4,702,903. Absorber rotor 11 then acts as a thermal rotaryregenerator, as in regenerative gas turbine engines having a compressor201 and an expander 220. Heat provided to the PSA process by heater 225assists powering the process according to a regenerative thermodynamicpower cycle, similar to advanced regenerative gas turbine enginesapproximately realizing the Ericsson thermodynamic cycle withintercooling on the compression side and interstage heating on theexpansion side. In the instance of PSA applied to oxygen separation fromair, the total light reflux flow is much less than the feed flow becauseof the strong bulk adsorption of nitrogen. Accordingly the powerrecoverable from the expanders is much less than the power required bythe compressor, but will still contribute significantly to enhancedefficiency of oxygen production.

If high energy efficiency is not of highest importance, the light refluxexpander stages and the countercurrent blowdown expander stages may bereplaced by restrictor orifices or throttle valves for pressure letdown.The schematic of FIG. 7 shows a single shaft supporting the compressorstages, the countercurrent blowdown or exhaust expander stages, and thelight reflux stages, as well as coupling the compressor to the primemover. However, it should be understood that separate shafts and evenseparate prime movers may be used for the distinct compression andexpansion stages within the scope of the present invention.

FIG. 8

FIG. 8 shows a vacuum-PSA system, also with heavy product reflux ascould be used to achieve high recovery in hydrogen purification for fuelcell power plant. The raw hydrogen may be provided in certain stationaryapplications from chemical process or petroleum refinery offgases.However, in most fuel cell applications, the raw hydrogen gas feed willbe provided by processing of a hydrocarbon or carbonaceous fuel, e.g. bysteam reforming of natural gas or methanol, or by autothermal reformingor partial oxidation of liquid fuels. Such hydrogen feed gases typicallycontain 30% to 75% hydrogen. Using typical adsorbents such as zeolites,carbon dioxide, carbon monoxide, nitrogen, ammonia, and hydrogen sulfideor other trace impurities will be much more readily adsorbed thanhydrogen, so the purified hydrogen will be the light product deliveredat the higher working pressure which may be only slightly less than thefeed supply pressure, while the impurities will be concentrated as theheavy product and will be exhausted from the PSA process as “PSA tailgas” at the lower working pressure. This tail gas will be used as fuelgas for the fuel processing reactions to generate hydrogen, or else fora combustion turbine to power PSA compression machinery for the fuelcell power plant.

The PSA system of FIG. 8 has infeed conduit 300 to introduce the feedgas at substantially the higher pressure to first feed manifold 53. Inthis example, all but the final pressurization steps are achieved withlight reflux gas, with the final feed pressurization step being achievedthrough manifold 55.

The PSA system includes a multistage vacuum pump 301 driven by primemover 209 through shaft 210, and optionally by light reflux expander 220through shaft 309. The vacuum pump 301 includes a first stage 302drawing heavy gas by conduit 246 from first product exhaust manifold 61,and compressing this gas through intercooler 303 to second stage 304.Vacuum pump second stage 304 draws heavy gas from second countercurrentblowdown manifold 59 through conduit 244, and delivers this gas byintercooler 305 to third stage 306 which also draws heavy gas from firstcountercurrent blowdown manifold 57 through conduit 240. The vacuum pumpstage 306 compresses the heavy gas to a pressure sufficiently aboveambient pressure for a portion of this gas (heavy product gas or PSAtail gas) to be delivered for use as fuel has in heavy product deliveryconduit 307. The remaining heavy gas proceeds from vacuum pump 301 toheavy reflux compressor 308 which attains substantially the higherworking pressure of the PSA cycle.

The compressed heavy gas is conveyed from compressor fourth stage 308 byconduit 310 to condensate separator 311. If desired (as for combustionin an expansion turbine as in the embodiment of FIG. 13), the entireheavy product stream could be compressed through compressor 308, so thatthe heavy product fuel gas may be delivered at the highest workingpressure by alternative heavy product delivery conduit 312 which isexternally maintained at substantially the higher pressure lessfrictional pressure drops. Condensed vapors (such as water) are removedthrough conduit 313 at substantially the same pressure as the heavyproduct in conduit 312. The remaining heavy gas flow, after removal ofthe first product, gas, flows by conduit 314 to the second feed manifold55 as heavy reflux to the adsorbers following the feed step for eachabsorber. The heavy reflux gas is a second feed gas, of higherconcentration in the more readily adsorbed component or fraction thanthe first feed gas.

FIGS. 9 and 10

Turning now to FIGS. 9 and 10, fuel cell-based electrical currentgenerating systems, according to a first embodiment of the presentinvention, are shown using a rotary PSA system similar to that shown inFIG. 7 as the basic building block. However, it should be understoodthat the invention is not limited to electrical current generatingsystems having rotary PSA modules. Rather other arrangements may beemployed without departing from the scope of the invention.

In FIG. 9, the PSA system separates oxygen from air, usingnitrogen-selective zeolite adsorbents, as previously described. Thelight product is concentrated oxygen, while the heavy product isnitrogen-enriched air usually vented as waste. The cycle lower pressure152 is nominally atmospheric pressure, unless an optional vacuum pump isprovided as in FIG. 8. Feed air is introduced through filter intake 200to a feed compressor 201. The feed compressor includes compressor firststage 202, compressor second stage 204, compressor third stage 206, andcompressor fourth stage 208. The feed compressor 201 as described may bea four stage axial compressor with motor 209 as prime mover coupled byshaft 210. The compressor stages may be in series as shown, oralternatively in parallel. Intercoolers between compressor stages areoptional. The feed compressor first and second stages deliver feed gasat the first intermediate feed pressure 161 via conduit 212 and watercondensate separator 213 to first feed pressurization manifold 48. Feedcompressor third stage 206 delivers feed gas at the second intermediatefeed pressure 163 via conduit 214 and water condensate separator 215 tosecond feed pressurization manifold 51. Feed compressor fourth stage 208delivers feed gas at the higher pressure 151 via conduit 216 and watercondensate separator 217 to feed manifold 53. Light product oxygen flowis delivered from light product manifold 71 by conduit 218, maintainedat substantially the higher pressure less frictional pressure drops.

The apparatus of FIG. 9 includes energy recovery expanders, includinglight reflux expander 220 (here including four stages) andcountercurrent blowdown expander 221 (here including two stages).Expander 221 is coupled to feed compressor 201 by shaft 222. Theexpander stages may be provided for example as radial inflow turbinestages, as full admission axial turbine stages with separate wheels, oras partial admission turbine stages combined in a single wheel. If highenergy efficiency were not of highest importance, the light refluxexpander stages and/or the countercurrent blowdown expander stages couldbe replaced by restrictor orifices or throttle valves for pressureletdown.

Light reflux gas from light reflux exit manifold 73 flows at the higherpressure via conduit 224 and heater 225 to first light reflux expanderstage 226, and then flows at the third light reflux pressurizationpressure 192 by conduit 227 to the first light reflux return manifold87. Light reflux gas from second light reflux exit manifold 75 flows atthe first concurrent blowdown pressure 171 via conduit 228 and heater225 to the second expander stage 230, and then flows at the second lightreflux pressurization pressure 191 by conduit 231 to the second lightreflux return manifold 85. Light reflux gas from third light reflux exitmanifold 77 flows at the second concurrent blowdown pressure 173 viaconduit 232 and heater 225 to the third expander stage 234, and thenflows at the first light reflux pressurization pressure 190 by conduit235 to the third light reflux return manifold 83. Finally, light refluxgas from fourth light reflux exit manifold 79 flows at the thirdconcurrent blowdown pressure 175 via conduit 236 and heater 225 tofourth light reflux expander stage 238, and then flows at substantiallythe lower pressure 152 by conduit 239 to the fourth light reflux returnmanifold 81.

Heavy countercurrent blowdown gas from first countercurrent blowdownmanifold 57 flows at first countercurrent blowdown intermediate pressure180 by conduit 240 to heater 241 and thence to first stage 242 of thecountercurrent blowdown expander 221, and is discharged from theexpander to exhaust manifold 243 at substantially the lower pressure152.

Optional heaters 225 and 241 raise the temperature of gases enteringexpanders 220 and 221, thus augmenting the recovery of expansion energyand increasing the power transmitted by shaft 222 from expanders 220 and221 to feed compressor 201, and reducing the power required from primemover 209.

In the instance of PSA applied to oxygen separation from air, the totallight reflux flow is much less than the feed flow because of the strongbulk adsorption of nitrogen. Accordingly the power recoverable from theexpanders is much less than the power required by the compressor, butwill still contribute significantly to enhanced efficiency of oxygenproduction. By operating the adsorbers at moderately elevatedtemperature (e.g. 40° to 60° C.) and using strongly nitrogen-selectiveadsorbents such as Ca-X, Li-X or lithium chabazite zeolites, the PSAoxygen generation system can operate with favorable performance andefficiency. Calcium or strontium exchanged chabazite may be used athigher temperatures, even in excess of 100° C., reflecting theextraordinary capacity of these adsorbents for nitrogen, their nitrogenuptake being too close to saturation at lower temperatures near ambientfor satisfactory operation.

While higher temperature of the adsorbent will reduce nitrogen uptakeand selectivity for each zeolite adsorbent, the isotherms will be morelinear and humidity rejection will be easier. Working with adsorbentssuch as Ca-X and Li-X, recent conventional practice has been to operateambient temperature PSA at subatmospheric lower pressures in so-called“vacuum swing adsorption” (VSA), so that the highly selective adsorbentsoperate well below saturation in nitrogen uptake, and have a largeworking capacity in a relatively linear isotherm range. At highertemperatures, saturation in nitrogen uptake is shifted to more elevatedpressures, so that optimum PSA cycle higher and lower pressures are alsoshifted upward.

The enriched oxygen product gas is delivered by conduit 218, non-returnvalve 250, and conduit 251 to the inlet of oxygen product compressor 252which boosts the pressure of product oxygen delivered by conduit 253.Compressor 252 may be a single stage centrifugal compressor, drivendirectly through shaft 254 by light reflux expander 220 or alternativelyby a motor. Light reflux expander 220 may be the sole power source tocompressor 252, in which case expander 220 and compressor 252 togetherconstitute a free rotor turbo-booster 255. Since the working fluid inboth expander 220 and compressor 252 is enriched oxygen, the free rotorturbo-booster embodiment has the important safety feature of notrequiring a shaft seal to an external motor. Preferably, energyrecovered from light reflux expansion is used to raise the deliverypressure of the light product, here oxygen.

The compressed enriched oxygen is delivered to a fuel cell 260, byconduit 253 to cathode inlet 261 of fuel cell cathode channel 262. Fuelcell 260 may be of the polymer electrolyte membrane (PEM), with theelectrolyte 265 separating cathode channel 262 from anode channel 266.Hydrogen fuel is supplied to anode inlet 267 of anode channel 266 byhydrogen infeed conduit 268.

The enriched oxygen passes through cathode channel 262 to cathode exit270, as a fraction of the oxygen reacts with hydrogen ions crossing themembrane to generate electrical power and reacting to form byproductwater. The cathode exit gas leaving the cathode channel in conduit 280from cathode exit 270 (in this preferred embodiment) is stillsignificantly enriched in oxygen relative to ambient air concentrationof approximately 21%. A minor portion of this gas is purged as cathodepurge gas from conduit 280 by purge valve 285 and purge exhaust 286, andthe balance of the cathode exit gas is retained as cathode recycle gas.The cathode recycle gas is conveyed by conduit 281 to water condensateseparator 282 where excess liquid water is removed from the cathode exitgas, which remains saturated in water vapor. The humid cathode recyclegas is then blended with incoming enriched oxygen form the PSA system byconduit 283 connecting to conduit 251.

Conduits 251, 253, 280, 281 and 283 thus form a cathode loop withcathode channel 262, compressor 252 and water condensate separator 282.Heat exchanger 225 may cool the oxygen-enriched gas to be compressed bycompressor 252, by removing waste heat from the fuel cell cathode loopto heat light reflux gas before expansion in expander 220. Enough of thecathode exit gas is purged by purge valve 285 to avoid excessivebuild-up of argon and nitrogen impurities in the cathode loop. In apracticable example, the product oxygen concentration in conduit 218 maybe 90% oxygen, with equal amounts of argon and nitrogen impurities. Witha small purge flow, oxygen concentrations at cathode inlet 261 and atcathode exit 270 may be respectively 60% and 50%.

As discussed above, a PEM fuel cell operating with atmospheric air asoxidant may typically require air compression to at least 3 atmospheresin order to achieve a sufficiently high oxygen partial pressure over thecathode for competitive current density in the fuel cell stack. Oxygenconcentration at the cathode inlet would be 21%, and at the cathode exittypically only about 10% oxygen. The present invention can achieve muchhigher average oxygen concentration over the fuel cell cathode channel,e.g. 55% compared to approximately 15%. Hence, the operating pressuremay be reduced to about 1.5 atmospheres while still retaining asubstantial enhancement of oxygen partial pressure over the cathode.With higher oxygen partial pressure over the cathode, fuel cell stackpower density and efficiency can be enhanced, as is particularly crucialin automotive power plant applications. Mechanical compression powerrequired by the apparatus of the present invention (using highperformance adsorbents such as Li-X) will be less than that required forthe air compressor of a PEM fuel cell system operating at 3 atmospheresair supply pressure, further enhancing overall power plant efficiency.

An important benefit in this example apparatus is that the oxygenenriched gas entering cathode inlet 261 is humidified by blending withthe much larger stream of saturated cathode recycle gas. Another benefitis that energy recovery from the PSA unit can be applied to boostpressure and drive recycle circulation in the cathode loop, while fuelcell waste heat can be applied to heat exchangers 225 and 241 to enhanceexpansion energy recovery in the PSA unit. Yet another benefit is thatsuitable cathode channel circulation flow velocities to assuresatisfactory water removal from PEM fuel cells are readily achieved.

While recycle of cathode gas has benefits as discussed above, it will beunderstood that the invention may also be practiced without any suchrecycle feature, so that the cathode gas from cathode exit 270 mayalternatively be either discharged to atmosphere or else removed toanother use such as assisting combustion within a fuel processor.

Another variation is to operate the oxygen PSA unit to deliver oxygen ata relatively high concentration (e.g. in the range of 60% to 95%, ormore preferably 70% to 90% oxygen concentration), while bypassing afraction of the compressed air feed from conduit 216 past the PSA moduleto blend directly with product oxygen in conduit 70, conduit 283 orconduit 253. In this approach, the blended bypass air and PSA oxygenproduct (plus any recycle cathode gas from cathode exit port 270) mayhave a mixed oxygen concentration in the range of e.g. 30% to 50% sothat a substantial benefit of partial oxygen enrichment over the fuelcell cathode is provided, while the size and power consumption of thePSA unit is reduced.

Turning to FIG. 10, an oxygen-separating PSA-based fuel cell system isshown, similar to the fuel cell system in FIG. 9, but with acountercurrent blowdown expander driving a free rotor exhaust vacuumpump. Thus, in FIG. 9 dashed line 290 represents an optional feed airbypass conduit 290 with a flow control valve 291, communicating betweencompressed air feed conduit 216 and conduit 283 in the cathode recycleloop. In the embodiment of FIG. 10, shaft 222 coupling thecountercurrent blowdown expander 221 to feed compressor 201 has beenremoved. Instead, vacuum pump 301 is used to depress the low pressure ofthe cycle below atmospheric pressure, drawing nitrogen-enriched wastegas from heavy product exhaust compartment 61 via conduit 246 andoptional heater 302. Pump 301 is powered by countercurrent blowdownexpander 304 expanding countercurrent blowdown gas from firstcountercurrent blowdown manifold 57 via conduit 240 and optional heater241. Vacuum pump 301 and expander 304 are coupled by shaft 305, andtogether constitute a free rotor vacuum pump assembly 306. Such a freerotor vacuum pump offers attractive advantages of efficiency and capitalcost. Alternatively, a motor could be coupled to an extension of shaft305.

The countercurrent blowdown gas from second countercurrent blowdownmanifold 59 exits that manifold at a pressure which is substantiallyatmospheric or slightly greater according to the amount of throttlingrestriction associated with conduit 244.

FIG. 11

FIG. 11 shows a fuel cell-based electrical current generating system,similar to the electrical current generating system of FIG. 9, butwithout light reflux energy recovery, and with a portion of oxygenenriched gas discharged from the fuel cell cathode being used for apressurization step. The illustrative four stages of light refluxpressure letdown are achieved irreversibly over adjustable orifices 350,351, 352 and 353, which respectively connect conduits 224 and 227, 228and 231, 232 and 235, and 236 and 239. Orifices 350, 351, 352 and 353are actuated through linkage 354 by actuator(s) 355. Adjustment of theorifices is desirable to enable turndown of the PSA apparatus tooperation at reduced cycle frequency and reduced flow rates when thefuel cell power plant is operated at part load.

The fuel cell has a cathode recycle loop defined (in the loop flowdirection) by water condensate separator 360, conduit 361 conveyingenriched oxygen to cathode channel inlet 261, cathode channel 262,conduit 362 conveying cathode exhaust gas from cathode channel exit 270to cathode recycle conduit 365 including cathode recycle blower 363 topressurize the cathode recycle gas for admission to condensate separator360. Separator 360 removes fuel cell water exhaust condensate from thecathode recycle loop, while also humidifying the dry concentrated oxygenadmitted from the PSA system conduit from conduit 218.

A portion of the cathode exhaust is removed from the conduit 362 byconduit 371, branching from cathode recycle conduit 365. This portion ofthe cathode exhaust gas is recycled to the feed end of the PSA (oralternatively vacuum-PSA) apparatus, and is conveyed by conduit 371 towater condensate separator 373 and thence to first pressurizationmanifold 48 communicating to the first valve face 21. A throttle valve373 may be provided in conduit 371 to provide a pressure letdown asrequired from the pressure at cathode exit 270 to first pressurizationmanifold 48.

Recycling a portion of the cathode exhaust gas to the PSA unit feed hasseveral advantages, including (1) reducing the volume of feed gas to becompressed, (2) eliminating the requirement to purge any cathode exhaustgas from the cathode loop, and (3) recovering some waste energy from thefuel cell cathode loop by using this gas to help pressurize the fuelcell from the feed end. This oxygen rich gas must be admitted to thefeed end of the PSA unit, because it is saturated with water vapor whichwould deactivate the adsorbent if admitted directly to the second valveface at the product end. By introducing it to the feed end of the bedsafter the low pressure step and before any direct pressurization withfeed air, a favorable concentration profile is established since thisgas is richer in oxygen than feed air, but also contains a greater loadof impurities than the product oxygen-enriched gas.

Because argon is concentrated with oxygen by the PSA unit, argon will beconcentrated both within the cathode loop and in the PSA enriched oxygenproduct in this embodiment. If no cathode purge is provided, argon canonly exit the system through the exhaust of the PSA unit. Since the PSAunit typically achieves about 60% recovery of oxygen and argon whenordinary air is used as the only feed for pressurization to the firstvalve face, about 40% of argon admitted with feed gas may be exhaustedin each cycle. The fractional elimination of recycle argon introducedwith initial feed pressurization steps will be lower, since the mainfeed is introduced subsequently to push the recycle argon deeper intothe absorbers. Hence, a small amount of purge from the cathode loop maybe desirable. Cathode exhaust gas recycle to the PSA unit feed may alsobe blended directly with feed air introduced at the same or lowerpressure as the cathode channel exit 270.

FIG. 12

FIG. 12 shows a fuel-cell based electrical current generating system400, according to a second embodiment of the present invention,comprising a fuel cell 402, an oxygen-generating PSA system 404, and ahydrogen gas production system 406. The fuel cell comprises an anodechannel 408 including an anode gas inlet 410 and an anode gas outlet412, a cathode channel 414 including a cathode gas inlet 416 and acathode gas outlet 418, and a PEM 420 in communication with the anodechannel 408 and the cathode channel 414 for facilitating ion exchangebetween the anode channel 408 and the cathode channel 414.

The oxygen-PSA system 404 extracts oxygen gas from feed air, andcomprises a rotary module 10, and a compressor 422 for deliveringpressurized feed air to the feed compartments 424 of the rotary module10. Preferably, the oxygen-PSA system 404 includes a vacuum pump 426 (oralternatively countercurrent blowdown expander) coupled to thecompressor 422 for withdrawing nitrogen-enriched gas as heavy productgas from the blowdown compartments 428 of the rotary module 10. Theoxygen-PSA system 404 also includes a light product gas functioncompartment 430 coupled to the cathode gas inlet 416 for deliveringoxygen-enriched gas to the cathode channel 414. Cathode recycle may beprovided as in the embodiments of FIGS. 9-11.

The hydrogen gas production system 406 comprises a hydrogen-generatingPSA system 432, and a fuel processor reactor 434 coupled to thehydrogen-PSA system 432 for supplying a first hydrogen gas feed to thehydrogen-PSA system 432. The hydrogen-PSA system 432 comprises a rotarymodule 10 including a first feed gas compartment 436 for receiving afirst hydrogen gas feed from the reactor 434, a pressurizationcompartment 438 for receiving a hydrogen gas feed from the anode gasoutlet 412, a light product compartment 440 for delivering hydrogen gasto the anode gas inlet 410, and a blowdown compartment 441 fordelivering tail gas as heavy product gas to the reactor 434. Preferablythe hydrogen-PSA system 432 includes a vacuum pump 442 (or alternately acountercurrent blowdown expander) provided between the blowdowncompartment 441 and the reactor 434 for extracting the tail gas from theblowdown compartment 441.

According to the purity level of the hydrogen gas recycled from theanode gas exit 412, pressurization compartment 438 may cooperate witheither the first or second valve of the rotary module, the latter beingpreferred if the purity of this stream is relatively high. Thehydrogen-PSA system 432 may also include a heavy reflux compressor 443delivering heavy reflux gas to a second feed gas compartment 444 toimprove the fractional recovery of hydrogen gas. The calorific fuel gasrequirements of the hydrogen gas production system 406 will determinethe correct recovery of hydrogen gas.

The reactor 434 comprises a steam reformer 445, including a burner 446and catalyst tubes (not shown), and a water gas shift reactor 448. Theburner 446 includes a first burner inlet 450 for receiving the tail gasfrom the blowdown compartment 442, and a second burner inlet 452 forreceiving air or humid oxygen-enriched gas from the cathode channel 414.The steam reformer 444 is supplied through a fuel inlet 454 with ahydrocarbon fuel, such as methane gas, plus water at a feed pressurewhich is the working pressure of the fuel cell plus an allowance forpressure drops through the system 406. The fuel is preheated and steamis generated by heat exchanger 455, recovering heat from the flue gas ofburner 446. The methane fuel gas and steam mixture is them passedthrough the catalyst tubes, while the tail gas and the oxygen-enrichedgas are burned in the burner 446 to elevate the temperature of themethane fuel gas mixture to the temperature necessary (typically 800°C.) for conducting endothermic steam reforming reactions of the methanefuel gas mixture:

 CH₄+H₂O−CO+3H₂CH₄+2H₂O−CO₂+4H₂

The resulting syngas (approximately 70% H₂, with equal amounts of CO andCO₂ as major impurities, and unreacted CH₄ and N₂ as minor impurities)is cooled to about 250° C., and then passed to the water gas shiftreactor 448 for reacting most of the CO with steam to produce more H₂and CO₂:CO+H₂O−CO₂+H₂

The resulting gas reactants are then conveyed to the first feedcompartment 436 of the hydrogen-PSA system 432 for hydrogenpurification, with the heavy product tail gas being returned to thesteam reformer 434 form the blowdown compartment 442 for combustion inthe burner 446.

In one variation, the reactor 434 comprises a partial oxidation reactor,and instead of the methane gas mixture being steam reformed, the methanegas mixture is reacted in the partial oxidation reactor with a portionof the humid oxygen-enriched gas received from the cathode channel 414,through an optional conduit 456, for partial oxidation of the methanegas:CH₄+½O₂−CO+2H₂

The resulting syngas is again cooled to about 250° C., and then passedto the water gas shift reactor 448 for reacting most of the CO withsteam to produce more H₂ and CO₂:CO+H₂O−CO₂+H₂

The resulting gas reactants are then conveyed to the first feedcompartment 436 of the hydrogen-PSA system 432 for hydrogenpurification, with the heavy product tail gas being purged from thehydrogen-PSA system 432.

In another variation, the reactor 434 comprises as autothermal reformerand a water gas shift reactor 448, and instead of the methane gasmixture being endothermically steam reformed or exothermically partiallyoxidized, the methane gas mixture is reacted in the autothermal reformerby a thermally balanced combination of those reactions, followed byreaction in the water gas shift reactor 448. Since the hydrogen-PSAheavy product tail gas will always have some fuel value even in thelimit of very high heavy reflux, a burner 446 would be provided forefficiently preheating air and or fuel feeds to any autothermal reactor.Unless the fuel processing reactions include an endothermic reformingcomponent as an energy-efficient sink for tail gas fuel combustion,another economic use (as in embodiment of FIG. 13) should be provided ifthe net fuel processing reactions are highly endothermic, as in the caseof simple partial oxidation.

Oxygen enrichment autothermal or partial oxidation fuel processoradvantageously reduces the heating load of reactants entering thereaction chamber, and also reduces the cooling load of hydrogen-richproduct gases delivered to the hydrogen PSA unit and the fuel cellanode, owing to the depletion of nitrogen from those gas streams. Afurther advantage of the present invention is the ability of thehydrogen PSA unit to remove ammonia in addition to carbon monoxide andhydrogen sulfide, which contaminants are all extremely detrimental toPEM fuel cell performance and life expectancy. Ammonia may be formed infuel processors where hydrocarbons are catalytically reformed tohydrogen in the presence of any atmospheric nitrogen. The oxygen PSAreduces this problem by front-end removal of nitrogen, while thehydrogen PSA removes any residual traces of ammonia.

FIG. 13

It would be apparent that a deficiency of the electrical currentgenerating system 400 relates to the necessity of driving the compressor422 and the vacuum pumps 426, 444 with a portion of the electrical powergenerated by the fuel cell. FIG. 13 shows a fuel cell based electricalcurrent generating system 500, which addresses this deficiency.

The electrical current generating system 500 is substantially similar tothe electrical current generating system 400, comprising the fuel cell402, an oxygen-generating PSA system 504, and a hydrogen gas productionsystem 506. The oxygen-PSA system 504 extracts oxygen gas from feed air,and comprises a rotary module 10, a compressor 522 for deliveringpressurized feed air to the feed compartments 524 of the rotary module10, a combustion expander 523 coupled to the compressor 522, a startermotor (not shown) coupled to the compressor 522, and a light product gasfunction compartment 530 coupled to the cathode gas inlet 416 fordelivering oxygen-enriched gas to the cathode channel 414. Theoxygen-PSA system 504 may also have a countercurrent blowdown or heavyproduct exhaust compartment 531 cooperating with a vacuum pump and/orexpander, as illustrated in previous embodiments.

The hydrogen gas production system 506 comprises a hydrogen-generatingPSA system 532, and a reactor 534 coupled to the hydrogen-PSA system forsupplying a first hydrogen gas feed to the hydrogen-PSA system 532. Thehydrogen-PSA system 532 comprises a rotary module 10 including a firstfeed gas compartment 536 for receiving a first hydrogen gas feed fromthe steam reformer 534, a pressurization compartment 538 (communicatingwith either the first or second valve) for receiving a second hydrogengas feed from the anode gas outlet 412, a light product compartment 540for delivering hydrogen gas to the anode gas inlet 410, and a blowdowncompartment 541 for delivering tail gas as heavy product fuel gas to thereactor 534. As in previous embodiments, the blowdown compartment 541may cooperate with an exhaust vacuum pump and/or expander (not shown)for extracting the tail gas from the blowdown compartment 541.

The reactor 534 comprises an autothermal reformer 544, a burner 546, anda water gas shift reactor 548. The burner 546 includes heater tubes 549,a first burner inlet 550 for receiving the tail gas from the blowdowncompartment 542, and a second burner inlet 552 for receiving compressedair from the compressor 522 second stage. As will be apparent from FIG.13, the compressor 522 second stage compresses a portion of the feed airwhich is not delivered to the oxygen-generating PSA system 504.

The expander 523 and the compressor 522 together comprise a gas turbine,and expands combustion product gas emanating from the burner 546 so asto increase the pressure of feed air to the feed compartments 524. Aswill be appreciated, the thermal energy of combustion of thehydrogen-PSA tail gas is used to drive the fuel cell accessory gaspurification and compression machinery. As shown in FIG. 13, additionalfeed gas compression energy may be obtained from the exothermic heat ofreaction of the water gas shift reactor 548 through preheat exchangers555.

The autothermal reformer 544 is supplied through a fuel inlet 554 with ahydrocarbon fuel gas, such as methane gas and, in the example shown, isreacted with oxygen-enriched gas received under pressure from thecathode channel 414 through booster blower 556. Cathode recycle may notbe justified, or at least may be reduced, if the oxygen-enriched gasdelivered from the cathode exit can be used advantageously for fuelprocessing (to reduce nitrogen load and enhance combustion). Theresultant syngas is then cooled, and then passed to the water gas shiftreactor 548 for reacting most of the CO with steam to produce more H₂and CO₂. The resulting gas reactants are then conveyed to the first feedcompartment 536 of the hydrogen-PSA system 532 for hydrogenpurification.

In some embodiments, at least a portion of the cathode exhaust gas(which is still enriched in oxygen relative to ambient air, and carriesfuel cell exhaust water and fuel cell waste heat) is returned to theinlet of an autothermal or partial oxidation fuel processor (orreformer) for reacting a hydrocarbon fuel with oxygen and steam in orderto generate raw hydrogen or syngas. The oxygen reacts autothermally witha portion of the fuel to produce carbon monoxide and heat which furthersreaction of remaining fuel with steam to generate hydrogen. Excess steamhelps prevent any coking in the reformer or fuel processor, andsubsequently reacts at lower temperature with the carbon monoxide in awater gas shift reactor to generate more hydrogen mixed with wastecarbon dioxide. Residual carbon monoxide, the carbon dioxide and anyother impurities can then be removed by a hydrogen PSA unit according tothe invention.

Delivery of still enriched oxygen gas from the fuel cell cathode to theinlet of the fuel processor (1) reduces the inert load of nitrogenentrained with atmospheric air as oxidant, (2) enhances circulationvelocities within the fuel cell cathode channel for effective waterremoval, (3) directly recovers exhaust water from the cathode for thefuel processor in direct accordance with water demand for fuelprocessing, (4) delivers that water largely in vapor form to avoidcostly condensation and revaporization steps, (5) delivers some fuelcell waste heat usefully to the fuel processor inlet, and (3) enhancesoverall system efficiency through desirable thermal integration.

FIG. 14

Embodiment 600 illustrates further aspects of the invention. Foralkaline fuel cells, the crucial problem is removal of CO₂ from bothfeed oxidant and hydrogen streams. The oxygen-PSA and hydrogen-PSAsystems of this invention as described above will remove CO₂ veryeffectively, since CO₂ is much more strongly adsorbed than otherpermanent gas impurities. Oxygen enrichment is beneficial for all typesof fuel cells in increasing voltage efficiency, although not usuallyjustified except at high current densities. Alkaline fuel cells can usean under-sized oxygen-PSA for very effective carbon dioxide removalalong with modest oxygen enrichment, or may use the same PSA device withan adsorbent lacking nitrogen/oxygen selectivity (e.g. activated carbon,or high silica zeolites) for carbon dioxide clean-up without oxygenenrichment. The rotary PSA module and compression machinery of thisinvention for entirely suitable for this role.

Alkaline fuel cells operating on ambient air feed typically operate nearatmospheric pressure, at about 70° C. Under such conditions, the watervapor saturated cathode exhaust stream of nitrogen-enriched air servesto remove fuel cell product water while maintaining electrolyte waterbalance. Operation of alkaline fuel cells at higher temperature may bedesirable for high efficiency with less costly electrocatalystmaterials, or else for thermal integration to a methanol reformer usingfuel cell waste heat to vaporize reactants and even drive theendothermic reaction. But with increasing stack exhaust temperatures,operation with ambient air composition may rapidly become impracticable.At higher temperatures, the nitrogen rich cathode exhaust simply carriestoo much water vapor out of the system, unless the total pressure isuneconomically raised or else a condenser for water recovery isincluded.

With oxygen enrichment, the volume of the cathode exhaust can beadjusted to achieve water balance for any alkaline fuel cell. Reasonablelow stack working pressures become practicable, e.g. about 3 atmospheresfor a cathode exit temperature of 120° C. If oxygen enrichment iscarried out to the full capability of oxygen-PSA, e.g. approaching 95%oxygen purity, the cathode exhaust stream becomes dry steam with amodest concentration of permanent gases. This steam product may beuseful for diverse applications, including fuel processing ofhydrocarbon feedstocks to generate hydrogen.

Embodiment 600 shows an oxygen-PSA (also performing CO₂ removal) asshown in FIG. 12. The hydrogen side of the system is simplified in thisexample to show only the anode gas inlet of pure hydrogen. Oxygen atmore than 90% purity is supplied to the cathode gas inlet 416, whileconcentrated water vapor is delivered from cathode gas exit 418 andconveyed directly to steam expander 610. Expander 610 discharges tovacuum condenser 612, from which liquid condensate is removed by pump614, while the permanent gas overheads are withdrawn through conduit byvacuum pump 426 of the oxygen-PSA. Expander 610 may assist motor 616 todrive the compression machinery of the oxygen-PSA, thus improvingoverall efficiency of the fuel power plant by approximately 2 to 3%.

A final aspect of the invention (for any type of fuel cell) is theoptional provision of light product gas accumulators for the PSA units,and particularly for the oxygen-PSA as illustrated in FIG. 14. Oxygenproduct accumulator 660 includes an oxygen storage vessel 661 chargedfrom the light product compartment 430 through non-return valve 662, atsubstantially the upper pressure of the PSA process or optionally at anelevated pressure generated by a small accumulator charging compressor663. A peaking oxygen delivery valve 665 and a backflush valve 666 areprovided on either side of non-return valve 667 so as to enable oxygendelivery from the storage vessel respectively forward to the fuel cellcathode inlet or backward to the oxygen-PSA unit.

The oxygen storage vessel is charged during normal operation,particularly during intervals of stand-by or idling when the oxygen-PSAattains highest oxygen purity. The optional charging compressor may beoperated when the plant is idling, or (in vehicle applications) as anenergy load application of regenerative braking. The peaking oxygendelivery valve 665 is opened during intervals of peak power demand, soas to increase supply of concentrated oxygen to the cathode when mostneeded. If the oxygen accumulator is large enough, the oxygen-PSAcompressor 422 and vacuum pump 426 could be idled during brief intervalsof peak power demand, so as to release the power normally consumed byinternal accessories to meet external demand. Then, the size of the fuelcell stack (in a power plant required to meet occasional specified peakpower levels) can be reduced for important cost savings.

When the fuel cell power plant is shut down, the oxygen-PSA compressor422 is stopped first to drop the internal pressure for an initialblowdown of all absorbers. Then, backflush valve 666 is opened torelease a purging flow of oxygen to displace adsorbed nitrogen and someadsorbed water vapor from the absorbers over a short time interval. Theabsorbers are then left precharged with dry oxygen at atmosphericpressure, thus enabling fast response of the oxygen-PSA for the nextplant start-up.

FIGS. 15-21

FIG. 15 shows a rotary PSA module 701 configured for axial flow andparticularly suitable for smaller scale oxygen generation and hydrogenpurification. Module 701 includes a number “N” of adsorbers 703 inabsorber housing body 704. Each absorber has a first end 705 and asecond end 706, with a flow path therebetween contacting anitrogen-selective adsorbent. The adsorbers are deployed in anaxisymmetric array about axis 707 of the absorber housing body. Thehousing body 704 is in relative rotary motion about axis 707 with firstand second functional bodies 708 and 709, being engaged across a firstvalve face 710 with the first functional body 708 to which feed air issupplied and from which nitrogen-enriched air is withdrawn as the heavyproduct, and across a second valve face 711 with the second functionalbody 709 from which oxygen-enriched air is withdrawn as the lightproduct.

In preferred embodiments as particularly depicted in FIGS. 15-21, theadsorber housing 704 rotates and shall henceforth be referred to as theadsorber rotor 704, while the first and second functional bodies arestationary and together constitute a stator assembly 721 of the module.The first functional body shall henceforth be referred to as the firstvalve stator 708, and the second functional body shall henceforth bereferred to as the second valve stator 709.

In the embodiment shown in FIGS. 15-21, the flow path through theadsorbers is parallel to axis 707, so that the flow direction is axial,while the first and second valve faces are shown as flat annular discsnormal to axis 707. However, more generally the flow direction in theadsorbers may be axial or radial, and the first and second valve facesmay be any figure of revolution centred on axis 707. The steps of theprocess and the functional compartments to be defined will be in thesame angular relationship regardless of a radial or axial flow directionin the adsorbers.

FIGS. 15-21 are cross-sections of module 701 in the planes defined byarrows 712-713, 714-715, and 716-717. Arrow 720 in each section showsthe direction of rotation of the rotor 704.

FIG. 16 shows section 712-713 across FIG.15, which crosses the absorberrotor. Here, “N”=72. The adsorbers 703 are mounted between outer wall721 and inner wall 722 of absorber rotor 704. Each absorber comprises arectangular flat pack 703 of adsorbent sheets 723, with spacers 724between the sheets to define flow channels here in the axial direction.Separators 725 are provided between the adsorbers to fill void space andprevent leakage between the adsorbers. Other preferred configurationsfor the absorber module may be provided by forming the adsorbent sheetsand intervening spacers in trapezoidal packs or spiral rollsconstituting each absorber.

Alternatively the entire absorber rotor may be formed as a spiral rollof one adsorbent sheet or a plurality of adsorbent sheets, the spiralroll formed concentric with the axis 707 and with spacers betweenadjacent layers of the spirally rolled adsorbent sheet(s), and with atleast some of the spacers at narrow angular intervals extending alongthe entire length between the first and second ends as barriers totransverse flow, so as to partition the spiral roll into many channels,each of which serves as a distinct absorber. The first and second endsof the spiral roll would directly coincide with the first and secondvalve faces respectively.

The adsorbent sheets comprise a reinforcement material, in preferredembodiments glass fibre, metal foil or wire mesh, to which the adsorbentmaterial is attached with a suitable binder. For air separation toproduce enriched oxygen, typical adsorbents are X, A or chabazite typezeolites, typically exchanged with lithium, calcium, strontium,magnesium and/or other cations, and with optimized silicon/aluminiumratios as well known in the art. The zeolite crystals are bound withsilica, clay and other binders, or self-bound, within the adsorbentsheet matrix.

Satisfactory adsorbent sheets have been made by coating a slurry ofzeolite crystals with binder constituents onto the reinforcementmaterial, with successful examples including nonwoven fibreglass scrims,woven metal fabrics, and expanded aluminium foils. Spacers are providedby printing or embossing the adsorbent sheet with a raised pattern, orby placing a fabricated spacer between adjacent pairs of adsorbentsheets. Alternative satisfactory spacers have been provided as wovenmetal screens, non-woven fibreglass scrims, and metal foils with etchedflow channels in a photolithographic pattern.

Typical experimental sheet thicknesses have been 150 microns, withspacer heights in the range of 100 to 150 microns, and absorber flowchannel length approximately 20 cm. Using X type zeolites, excellentperformance has been achieved in oxygen separation from air at PSA cyclefrequencies in the range of 30 to 150 cycles per minute.

FIG. 17 shows the porting of rotor 704 in the first and second valvefaces respectively in the planes defined by arrows 714-715, and 716-717.An absorber port 730 provides fluid communication directly from thefirst or second end of each absorber to respectively the first or secondvalve face.

FIG. 18 shows the first stator valve face 800 of the first stator 708 inthe first valve face 710, in the plane defined by arrows 714-715. Fluidconnections are shown to a feed compressor 801 inducting feed air frominlet filter 802, and to an exhauster 803 delivering nitrogen-enrichedsecond product to a second product delivery conduit 804. Compressor 801and exhauster 803 are shown coupled to a drive motor 805.

Arrow 720 indicates the direction of rotation by the absorber rotor. Inthe annular valve face between circumferential seals 805 and 806, theopen area of first stator valve face 800 ported to the feed and exhaustcompartments is indicated by clear angular segments 811-816corresponding to the first functional ports communicating directly tofunctional compartments identified by the same reference numerals811-816. The substantially closed area of valve face 800 betweenfunctional compartments is indicated by hatched sectors 818 and 819which are slippers with zero clearance, or preferably a narrow clearanceto reduce friction and wear without excessive leakage. Typical closedsector 818 provides a transition for an absorber, between being open tocompartment 814 and open to compartment 815. Gradual opening is providedby a tapering clearance channel between the slipper and the sealingface, so as to achieve gentle pressure equalization of an absorber beingopened to a new compartment. Much wider closed sectors (e.g. 819) areprovided to substantially close flow to or from one end of the adsorberswhen pressurization or blowdown is being performed from the other end.

The feed compressor provides feed air to feed pressurizationcompartments 811 and 812, and to feed production compartment 813.Compartments 811 and 812 have successively increasing working pressures,while compartment 813 is at the higher working pressure of the PSAcycle. Compressor 801 may thus be a multistage or split streamcompressor system delivering the appropriate volume of feed flow to eachcompartment so as to achieve the pressurization of adsorbers through theintermediate pressure levels of compartments 811 and 812, and then thefinal pressurization and production through compartment 813. A splitstream compressor system may be provided in series as a multistagecompressor with interstage delivery ports; or as a plurality ofcompressors or compression cylinders in parallel, each delivering feedair to the working pressure of a compartment 811 to 813. Alternatively,compressor 801 may deliver all the feed air to the higher pressure, withthrottling of some of that air to supply feed pressurizationcompartments 811 and 812 at their respective intermediate pressures.

Similar, exhauster 803 exhausts nitrogen-enriched heavy product gas fromcountercurrent blowdown compartments 814 and 815 at the successivelydecreasing working pressures of those compartments, and finally fromexhaust compartment 816 which is at the lower pressure of the cycle.Similarly to compressor 801, exhauster 803 may be provided as amultistage or split stream machine, with stages in series or in parallelto accept each flow at the appropriate intermediate pressure descendingto the lower pressure.

In the example embodiment of FIG. 18, the lower pressure is ambientpressure, so exhaust compartment 816 exhaust directly to heavy productdelivery conduit 804. Exhauster 803 thus provides pressure letdown withenergy recovery to assist motor 805 from the countercurrent blowdowncompartments 814 and 815. For simplicity, exhauster 803 may be replacedby throttling orifices as countercurrent blowdown pressure letdown meansfrom compartments 814 and 815.

In some preferred embodiments, the lower pressure of the PSA cycle issubatmospheric. Exhauster 803 is then provided as a vacuum pump, asshown in FIG. 19. Again, the vacuum pump may be multistage or splitstream, with separate stages in series or in parallel, to acceptcountercurrent blowdown streams exiting their compartments at workingpressures greater than the lower pressure which is the deepest vacuumpressure. In FIG. 19, the early countercurrent blowdown stream fromcompartment 814 is released at ambient pressure directly to heavyproduct delivery conduit 804. If for simplicity a single stage vacuumpump were used, the countercurrent blowdown stream from compartment 815would be throttled down to the lower pressure over an orifice to jointhe stream from compartment 816 at the inlet of the vacuum pump.

FIGS. 20 and 21 shows the second stator valve face, at section 716-717of FIG. 15. Open ports of the valve face are second valve function portscommunicating directly to a light product delivery compartment 821; anumber of light reflux exit compartments 822, 823, 824 and 825; and thesame number of light reflux return compartments 826, 827, 828 and 829within the second stator. The second valve function ports are in theannular ring defined by circumferential seals 831 and 832. Each pair oflight reflux exit and return compartments provides a stage of lightreflux pressure letdown, respectively for the PSA process functions ofsupply to backfill, full or partial pressure equalization, andconcurrent blowdown to purge.

Illustrating the option of light reflux pressure letdown with energyrecovery, a split stream light reflux expander 840 is shown in FIGS. 15and 20 to provide pressure let-down of four light reflux stages withenergy recovery. The light reflux expander provides pressure let-downfor each of four light reflux stages, respectively between light refluxexit and return compartments 822 and 829, 823 and 828, 824 and 827, and825 and 826 as illustrated. The light reflux expander 840 may power alight product booster compressor 845 by drive shaft 846, which deliversthe oxygen enriched light product to oxygen delivery conduit 847 andcompressed to a delivery pressure above the higher pressure of the PSAcycle. Illustrating the option of light reflux pressure letdown withenergy recovery, a split stream light reflux expander 840 is provided toprovide pressure let-down of four light reflux stages with energyrecovery. The light reflux expander serves as pressure let-down meansfor each of four light reflux stages, respectively between light refluxexit and return compartments 822 and 829, 823 and 828, 824 and 827, and825 and 826 as illustrated.

Light reflux expander 840 is coupled to a light product pressure boostercompressor 845 by drive shaft 846. Compressor 845 receives the lightproduct from conduit 725, and delivers light product (compressed to adelivery pressure above the higher pressure of the PSA cycle) todelivery conduit 250. Since the light reflux and light product are bothenriched oxygen streams of approximately the same purity, expander 840and light product compressor 845 may be hermetically enclosed in asingle housing which may conveniently be integrated with the secondstator as shown in FIG. 15. This configuration of a “turbocompressor”oxygen booster without a separate drive motor is advantageous, as auseful pressure boost of the product oxygen can be achieved without anexternal motor and corresponding shaft seals, and can also be verycompact when designed to operate at very high shaft speeds.

FIG. 21 shows the simpler alternative of using a throttle orifice 850 asthe pressure letdown means for each of the light reflux stages.

Turning back to FIG. 15, compressed feed air is supplied to compartment813 as indicated by arrow 825, while nitrogen enriched heavy product isexhausted from compartment 817 as indicated by arrow 826. The rotor issupported by bearing 860 with shaft seal 861 on rotor drive shaft 862 inthe first stator 708, which is integrally assembled with the first andsecond valve stators. The absorber rotor is driven by motor 863 as rotordrive means.

As leakage across outer circumferential seal 831 on the second valveface 711 may compromise enriched oxygen purity, and more importantly mayallow ingress of atmospheric humidity into the second ends of theadsorbers which could deactivate the nitrogen-selective adsorbent, abuffer seal 870 is provided to provide more positive sealing of a bufferchamber 871 between seals 831 and 871. A desiccant 873 (e.g. alumina,silica gel, sodium hydroxide, potassium hydroxide, magnesiumperchlorate, barium oxide, phosphorous pentoxide, calcium chloride,calcium sulfate, calcium oxide, or magnesium oxide) may be included inbuffer chamber 871 to provide more moisture protection. Even though theworking pressure in some zones of the second valve face may besubatmospheric (in the case that a vacuum pump is used as exhauster803), buffer chamber is filled with dry enriched oxygen product at abuffer pressure positively above ambient pressure. Hence, minor leakageof dry oxygen outward may take place, but humid air may not leak intothe buffer chamber. In order to further minimize leakage and to reduceseal frictional torque, buffer seal 871 seals on a sealing face 872 at amuch smaller diameter than the diameter of circumferential seal 831.Buffer seal 870 seals between a rotor extension 875 of absorber rotor704 and the sealing face 872 on the second valve stator 709, with rotorextension 875 enveloping the rear portion of second valve stator 709 toform buffer chamber 871. A stator housing member 880 is provided asstructural connection between first valve stator 8 and second valvestator 709.

FIG. 22

FIG. 22 shows an axial section of a rotary PSA embodiment, in which theadsorbers and absorber body housing 904 are stationary, while the firstand second distributor valve bodies are first valve rotor 908 and secondvalve rotor 909 respectively engaged with first valve face 910 andsecond valve face 911. The first valve rotor 908 is driven by motor 1063through shaft 1062, while the second valve rotor 9 is driven byconnecting shaft 1110. As the arrows 720 in FIGS. 16-21 indicate thedirection of relative motion of the absorber housing 904 relative to thedistributor valve bodies, the rotation of valve rotors 908 and 909 forthe stationary absorber embodiment of FIG. 22 may be in the oppositedirection to arrows 720 when referred to the stationary housing 904. Thefirst valve rotor 908 is installed within first valve housing 1112, andsecond valve rotor 909 is installed within second valve housing 214.Housings 1112 and 1114 are assembled with absorber housing 904 to form acomplete pressure containment enclosure for the PSA module 901.

Alternative valve configurations and pressure balancing devices for thefirst and second rotating distributor valves for embodiments withstationary adsorbers are disclosed by Keefer et al in U.S. Pat. No.6,063,161, the disclosure of which is incorporated herein.

For all externally connected flow functions where feed is provided tothe first valve body, exhaust is withdrawn from the first valve body, orgas is withdrawn from or returned to the second valve body, fluidtransfer chambers are provided for each such flow function, in order toestablish fluid communication from the housing to the rotor for thatfunction. Each fluid transfer chamber is an annular cavity in the valverotor or its housing, providing fluid communication at all angularpositions of the rotor between a functional compartment in the rotor andthe corresponding external conduit connected to the housing. Rotaryseals must be provided for each such fluid transfer chamber to preventleakage. A particular advantage of rotary absorber embodiments is theelimination of such fluid transfer chambers and associated seals, sincein those embodiments the first and second valve bodies are stationaryand may be connected directly to external flow functions.

A feed transfer chamber 1120 communicates between feed conduit 1081 andfunctional compartment 1013 in the first valve rotor 908, and an exhausttransfer chamber 1122 communicates to exhaust conduit 1082 andfunctional compartment 1016 in the first valve rotor 908. Transferchambers 1120 and 1122 are separated by rotary seal 1124. Thisconfiguration is suitable for a single stage feed compressor 1001 and asingle stage exhauster 1003. Narrow clearance gaps in first valve face910 may extend from compartment 1013 over the annular sectorscorresponding to compartments 812 and 811 in FIGS. 18 and 19, and fromcompartment 1016 over the annular sectors corresponding to compartments815 and 814 in FIGS. 18 and 19, so as to provide throttling for gentlepressurization and depressurization of each absorber being opened tocompartments 1013 or 1016. While additional transfer chambers could beprovided for additional compression or exhaust stages, it will beappreciated that this complication could be avoided with rotary absorberembodiments.

A product transfer chamber 1126 communicates between product deliveryconduit 1047 and functional compartment 1021 in the second valve rotor909. Rotary seal 1127 is provided for transfer chamber 1126. Additionaltransfer chambers could be provided in pairs for exit and return of eachlight reflux stage. This may be necessary if a light reflux expander 840is provided as shown in FIG. 20. However, it will be much simpler in thestationary absorber embodiments to avoid fluid transfer between thesecond valve rotor 909 and its housing 1114 for light reflux stages. Forstationary absorber embodiments, it will thus be preferred to usethrottle orifices 850 for pressure let-down of each light reflux stageas shown in FIG. 21, with these orifices 850 installed within rotor 909so that no fluid transfer between rotor 909 and housing 1114 is requiredfor light reflux. One such orifice 1050 is shown in FIG. 22, with theconnection to light reflux exit compartment 1025 being out of thesectional plane and accordingly not shown in the view of FIG. 22.

Axial Flow Oxygen Enrichment PSA Unit

The specific productivity and the yield of an axial flow rotary oxygenenrichment PSA module similar to module 701 of FIG. 15 was measured withair feed at 30° C. The module had a total volume of 18 L (not includingthe compressor, the vacuum pump, and the rotor drive motor), and acontained absorber volume of 8.2 L. Specific productivity is defined asnormal liters of contained product oxygen delivered per hour per literof absorber volume, and yield is defined as fractional recovery ofoxygen contained in the product from oxygen contained in the feed air.

Operating in a vacuum-PSA mode at a cycle frequency of 100 cycles/minutewith feed air compressed to 1.5 bars absolute and vacuum exhaust at 0.5bars absolute, oxygen product at 70% purity was obtained with specificproductivity of 1500 NL/L-hour, at a yield of 47%.

Operating in a vacuum-PSA mode at a cycle frequency of 100 cycles/minutewith feed air compressed to 1.5 bars absolute and vacuum exhaust at 0.5bars absolute, oxygen product at 70% was obtained with specificproductivity improved to 1650 NL/L-hour and yield improved to 50.5%.

Operating in a vacuum-PSA mode at a cycle frequency of 100 cycles/minutewith feed air compressed to 1.7 bars absolute and vacuum exhaust at 0.32bars absolute, oxygen product at 80% purity was obtained with a specificproductivity of 2500 NL/L-hour, at a yield of 56%.

Operating in a positive pressure PSA mode at a cycle frequency of 100cycles/minute with feed air compressed to 3 bars absolute and exhaust atatmospheric pressure, oxygen product at 80% purity was obtained with aspecific productivity of 1320 NL/L-hour, at a yield of 25.5%.

Operating in a positive pressure PSA mode at a cycle frequency of 100cycles/minute with feed air compressed to 3 bars absolute and exhaust atatmospheric pressure, oxygen product at 70% purity was obtained with aspecific productivity of 1750 NL/L-hour, at a yield of 33%.

For comparison, conventional oxygen industrial vacuum-PSA and PSAsystems using granular adsorbent operate at cycle frequencies of onlyabout 1 cycle/minute, achieving specific productivities of about 30NL/L-hour. Specific productivities in the range of 130 to 170 NL/L-hourhave been reported for a prior art rotary PSA device (See Vigor et al.,U.S. Pat. No. 5,658,370). Keller et al. (U.S. Pat. No. 4,354,859)achieved specific productivities for oxygen in the range of 210 to 270NL/L-hour by operating at cycle frequencies of 45 to 50 cycles/minutewith a granular absorber of 40 to 80 mesh zeolite.

The high specific productivities realized with the axial flow rotary PSAsystem of the disclosure are thus substantially better than prior artsystems, by one to two full orders of magnitude. High productivitiesfrom the disclosed compact PSA units are decisively important forautomobile fuel cell applications, as prior art devices are far toobulky and heavy to be considered for such applications.

It is to be noted that the extreme compactness of the PSA devicesprovided for fuel cell systems by the present invention is enabled byoperating at high cycle frequency (greater than 50 cycles per minute,and more preferably greater than 100 cycles per minute) with the dualenabling aspects of the rotary PSA mechanism and the adsorbent modulesformed of thin adsorbent sheets with narrow channels spacedtherebetween. At a specific productivity of 1500 NL/L-hour, the abovementioned PSA unit delivered about 200 NL/min of contained oxygen from amodule volume of only 16 L. This oxygen flow rate would suffice for a 40kW fuel cell, or for an even larger fuel cell if additional oxygen isprovided by blending bypass air with the PSA product oxygen.

Hydrogen Purification PSA

Hydrogen purification PSA is particularly advantageous because itsuccessfully removes impurities to a level that are not incompatiblewith PEM fuel cells. Such impurities include many compounds that areinherent to fossil fuel reforming or hydrogen recovery from chemicalplant off-gases. For example, several particularly problematiccompounds, such as ammonia, carbon monoxide, hydrogen sulfide, methanolvapor, and chlorine are removed effectively by PSA.

Methanol is a preferred feedstock for PEM fuel cells in stationary andautomotive applications. Steam reforming of methanol generates rawhydrogen or syngas containing hydrogen, carbon dioxide and significantlevels of carbon monoxide and unreacted methanol. The hydrogen PSA ofthe present disclosure has been tested on synthetic methanol syngascontaining approximately 1% carbon monoxide, methanol vapor, and watervapor along with carbon dioxide as the bulk impurity. Each of theimpurities was reduced below a concentration of 50 ppm.

Autothermal reforming, steam reforming or partial oxidation of otherhydrocarbons (e.g. natural gas, gasoline, or diesel fuel) invariablyproduces raw hydrogen or syngas containing carbon dioxide and frequentlynitrogen as bulk impurities, with carbon monoxide and frequentlyhydrogen sulfide as potentially harmful contaminants. All of theseimpurities can be adequately removed by the hydrogen PSA unit of thepresent disclosure.

The ability of the hydrogen PSA unit to remove severely harmfulcomponents such as carbon monoxide, methanol vapor and hydrogen sulfideis most important for PEM fuel cells, to extend their operating life,improve their reliability, and potentially also reduce their cost byenabling lower noble metal catalyst loadings on the fuel cellelectrodes.

The ability of the hydrogen PSA unit to remove bulk impurities such ascarbon dioxide and nitrogen allows the fuel cell to operate with a highpartial pressure of hydrogen and with a much smaller cathode purge flow,thus improving electrochemical energy conversion efficiency while alsoimproving hydrogen utilization within the fuel cell anode channel.

The foregoing description is intended to be illustrative of thepreferred embodiments of the present invention. Those of ordinary skillmay envisage certain additions, deletions and/or modifications to thedescribed embodiments which, although not specifically described orreferred to herein, do not depart from the spirit or scope of thepresent invention as defined by the appended claims.

1. An electrical current generating system, comprising: at least onefuel cell; and a hydrogen gas delivery system coupled to the fuel cellfor delivering hydrogen to the fuel cell, the hydrogen gas deliverysystem comprising a rotary pressure swing adsorption module, wherein therotary pressure swing adsorption module includes an adsorbent thatpreferentially adsorbs at least one carbon oxide.
 2. The systemaccording to claim 1, wherein the carbon oxide is carbon monoxide orcarbon dioxide.
 3. An electrical current generating system comprising: afuel cell including an anode channel including an anode gas inlet and ananode gas outlet, a cathode channel including a cathode gas inlet and acathode gas outlet, and an electrolyte in communication with the anodeand cathode channel for facilitating exchange between the anode andcathode channel; an oxygen gas delivery system coupled to the cathodegas inlet for delivering oxygen gas to the cathode channel; and ahydrogen gas delivery system coupled to the anode gas inlet fordelivering a gaseous stream enriched in hydrogen gas to the anodechannel, including a first rotary pressure swing adsorption system forenriching hydrogen in a gaseous feed, where the first rotary pressureswing adsorption system includes a first gas feed gas inlet forreceiving a first gas feed comprising hydrogen gas and a gas outletcoupled to the anode gas inlet.
 4. The system according to claim 3,wherein the first rotary pressure swing adsorption system includes anadsorbent that preferentially adsorbs at least one carbon oxide.
 5. Thesystem according to claim 4, wherein the carbon oxide is carbon monoxideor carbon dioxide.
 6. The electrical current generation system accordingto claim 3 where the hydrogen gas delivery system includes a gas inletfor receiving a second gas feed from the anode gas outlet and a gasoutlet for delivering the gaseous stream enriched in hydrogen gas to theanode channel.
 7. The electrical current generation system according toclaim 6 where the second gas feed is passed through the first rotarypressure swing adsorption system.
 8. The electrical current generationsystem according to claim 7 where the first rotary pressure swingadsorption system includes a second feed gas inlet for receiving thesecond gas feed.
 9. The electrical current generating system accordingto claim 8 where the hydrogen gas delivery system comprises a reactorfor producing the first gas feed from hydrocarbon fuel, and wherein thefirst rotary pressure swing adsorption system is coupled to the reactorfor receiving the first and second gas feeds.
 10. The electrical currentgenerating system according to claim 3 wherein the hydrogen gas deliverysystem comprises a reactor for producing the first hydrogen gas feedfrom hydrocarbon fuel.
 11. The electrical current generating systemaccording to claim 9 where the first rotary pressure swing adsorptionsystem hydrogen includes a first feed gas inlet for receiving the firstgas feed, and a second feed gas inlet for receiving the second gas feed.12. The electrical current generating system according to claim 11 wherethe first gas feed is provided at a pressure level different from apressure level of the second gas feed.
 13. The electrical currentgenerating system according to claim 9 where the reactor comprises asteam reformer, and a water gas shift reactor coupled to the steamreformer for producing the first gas feed.
 14. The electrical currentgenerating system according to claim 9 wherein the reactor comprises anautothermal reformer, and a water gas shifi reactor coupled to the steamreformer for producing the first gas feed.
 15. The electrical generatingsystem according to claim 3 further comprising a gas recirculation meanscoupled to the cathode gas outlet for recirculating a portion of cathodeexhaust gas exhausted from the cathode channel to the cathode gas inlet.16. The electrical generating system according to claim 9 furthercomprising a gas recirculation means coupled to the cathode gas outletfor recirculating a portion of cathode exhaust gas exhausted from thecathode channel to the reactor for producing hydrogen from hydrocarbonfuel.